The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 16, 2021

Filed:

Jan. 09, 2019
Applicant:

Innoveering, Llc, Ronkonkoma, NY (US);

Inventors:

Dean Modroukas, Scarsdale, NY (US);

Robert Bakos, Wading River, NY (US);

Assignee:

INNOVEERING, LLC, Bohemia, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B01J 19/00 (2006.01); F02C 7/22 (2006.01); B01J 19/26 (2006.01); F02K 7/16 (2006.01); F28F 1/12 (2006.01); B01J 12/00 (2006.01); F02K 7/10 (2006.01); F28D 7/10 (2006.01); B01J 19/24 (2006.01);
U.S. Cl.
CPC ...
B01J 19/0093 (2013.01); B01J 12/005 (2013.01); B01J 12/007 (2013.01); B01J 19/2485 (2013.01); B01J 19/26 (2013.01); F02C 7/22 (2013.01); F02K 7/10 (2013.01); F02K 7/16 (2013.01); F28D 7/106 (2013.01); F28F 1/128 (2013.01); B01J 2219/00835 (2013.01); B01J 2219/2428 (2013.01); B01J 2219/2429 (2013.01);
Abstract

A fuel reformation system includes a fuel delivery system that supports fuel, an oxidizer delivery system that supports an oxidizer, a mixer/vaporizer system in fluid communication with the fuel delivery system and the oxidizer delivery system, and a fuel processing reactor system. The mixer/vaporizer system receives the oxidizer from the oxidizer delivery system and the fuel from the fuel delivery system to mix and vaporize the oxidizer and fuel into a first effluent. The fuel processing reactor system receives the first effluent and reacts with the first effluent to generate a second effluent in the form of hot syngas for selective injection into a high speed, air-breathing propulsion system.


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